Nothing Special   »   [go: up one dir, main page]

US6679063B2 - Combustion chamber head for a gas turbine - Google Patents

Combustion chamber head for a gas turbine Download PDF

Info

Publication number
US6679063B2
US6679063B2 US09/968,491 US96849101A US6679063B2 US 6679063 B2 US6679063 B2 US 6679063B2 US 96849101 A US96849101 A US 96849101A US 6679063 B2 US6679063 B2 US 6679063B2
Authority
US
United States
Prior art keywords
combustion chamber
metering panel
heat shield
cooling air
sleeve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US09/968,491
Other versions
US20020038549A1 (en
Inventor
Michael Ebel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
Rolls Royce Deutschland Ltd and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce Deutschland Ltd and Co KG filed Critical Rolls Royce Deutschland Ltd and Co KG
Assigned to ROLLS-ROYCE DEUTSCHLAND LTD. & CO KG reassignment ROLLS-ROYCE DEUTSCHLAND LTD. & CO KG ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: EBEL, MICHAEL
Publication of US20020038549A1 publication Critical patent/US20020038549A1/en
Application granted granted Critical
Publication of US6679063B2 publication Critical patent/US6679063B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means

Definitions

  • This invention relates to a gas turbine with at least one combustion chamber, a combustion chamber wall, a metering panel, at least one heat shield, at least one sleeve and a cowling.
  • combustion chambers are of the one-part annular type made up of several, inseparably connected components.
  • the main components are the inner and the outer combustion chamber wall and the combustion chamber head.
  • the combustion chamber head is either made as a single component, for example by casting, or of different components, such as sheet-metal fabrications, turned parts etc.
  • combustion chamber heads are known which are made up of individual components joined together by bolt-type fastenings or similar means.
  • the known designs generally are characterized by a high assembly effort.
  • assembly of the heat shield together with the sleeves to the metering panel is difficult with some of the known designs since it must be performed from the exit side of the combustion chamber. This involves a considerable increase of the assembly costs.
  • combustion chamber heads have zones which are problematic in terms of the supply of cooling air, these problems arising from the circumstance that the individual components may compromise the supply of cooling air to the heat shield in certain zones.
  • the sleeve and the heat shield form a unit and are assembled together on the metering panel from the exit of the combustion chamber.
  • the surface of the sleeve which faces the combustion chamber interior is liable to considerable heating and cannot be cooled effectively.
  • the present invention provides a combustion chamber head of the type specified at the beginning which combines simplicity of design and easy and cost-effective manufacture and assembly with the capability of effective cooling of the heat shield.
  • a combustion chamber head for a gas turbine comprising: a combustion chamber outer wall; a combustion chamber inner wall; a metering panel; at least one heat shield; at least one sleeve; and a cowling; wherein the metering panel is formed as a unitary part with the combustion chamber outer wall and the combustion chamber inner wall, the heat shield is mounted to the metering panel from a downstream side of the metering panel, the sleeve is mounted to the metering panel from an upstream side of the metering panel, and the cowling is removably attached to the metering panel.
  • the combustion chamber head according to this invention is characterized by a variety of merits.
  • the heat shield is mounted to the metering panel from the downstream side, whilst all other components are fitted from the upstream side of the metering panel.
  • This method of assembly is far simpler since it dispenses with the need of fitting and securing bolt-type fastenings or similar means from the side of the combustion chamber interior.
  • the removable cowling provides for free, undisturbed access to the assembly areas. Providing the cowling as an extra, removable, separate component enables the entire combustion chamber head to be assembled without any problems. Moreover, it is not necessary to provide the cowling with assembly openings or similar means as known in the prior art. Rather, the present invention provides for free, unhindered access to the upstream side of the metering panel.
  • a particularly favourable feature of the design according to the present invention is that the sleeves are installed from the upstream side of the metering panel. This feature provides for re-location of the sliding and sealing face away from the metering panel, enabling cooling air to reach also the inner areas of the heat shield without problems. This provides for more effective and improved cooling.
  • the heat shield is provided with stud bolts which can be led through openings in the metering panel. Separate bolts or similar means are, therefore, dispensable. Attaching the stud bolts to the heat shield also ensures high operational safety by avoiding the risk of parts coming off and entering the combustion chamber interior during operation.
  • the sleeve is preferably attached by means of retainers on the metering panel.
  • these retainers are attached to the stud bolts of the heat shield. Additional bolts or threaded fastenings can, therefore, be entirely dispensed with. The entire construction is simplified considerably.
  • each retainer holds two adjacent sleeves.
  • At least one stud bolt is provided on the retainers.
  • the cowling can simply be put onto the studs and bolted from the exterior.
  • the metering panel is provided with a plurality of cooling air holes, as known in the state of the art.
  • the heat shield can be favourable to provide it with a rim which abuts a collar of the sleeve, this rim extending in the upstream direction and being led through an opening in the metering panel.
  • the height of the rim is selected such that, in the installed condition, the rim extends appropriately beyond the upstream side of the metering panel, thereby allowing the cooling air to freely access the central zone of the heat shield even if the collar of the sleeve abuts the cylindrical rim.
  • the design according to the present invention enables a defined gap to be provided between the outer wall of the cylindrical rim of the sleeve and the inner wall of the rim of the heat shield, this gap permitting a radial and circumferential relative movement of a fuel nozzle and the combustion chamber head.
  • the size of the collar of the sleeve exceeds the outer diameter of the rim of the heat shield by the max. possible amount of movement, this feature enabling the space before the metering panel to be sealed to the combustion chamber against undesired leakage air even if the max. possible movement of the sleeve should take place. This provides for advantageous assembly and operating conditions.
  • the gaps between the sleeve and the retainers are particularly advantageous since they provide for sufficient clearance necessary for thermal compensation.
  • the sleeve is securely and adequately positioned by the left or right part, respectively, of the adjacent retainers. Accordingly, each retainer secures two adjacent sleeves.
  • the retainer itself is fitted to the stud bolts of the heat shield and secured to the metering panel with appropriate nuts.
  • the retainer can accordingly also be designed as a support for the cowling, as already mentioned in the above.
  • the design proposed in the present invention enables the individual components to be separately manufactured and safely assembled. This provides for a high degree of flexibility also in terms of the candidate manufacturing processes and materials.
  • FIG. 1 is a design of a combustion chamber head in accordance with the state of the art
  • FIG. 2 is a simplified sectional side view of an embodiment of a combustion chamber according to the present invention with a combustion chamber head according to the present invention
  • FIG. 3 is an enlarged partial view of the combustion chamber head of FIG. 2,
  • FIG. 4 is a sectional view of a combustion chamber head showing multiple heat shields and sleeves
  • FIG. 5 is a perspective partial view similar to FIG. 4 of the upstream area of the metering panel with the multiple sleeves and retainers, and
  • FIG. 6 is a simplified sectional side view of the metering panel and the heat shield showing the attachment of the heat shield by means of stud bolts.
  • FIG. 1 shows the design according to the state of the art in which a combustion chamber outer wall 2 and a combustion chamber inner wall 3 forms a one-part design with a metering panel 1 . Also, the metering panel 1 forms one part with a cowling 6 .
  • a heat shield 4 is fastened to the metering panel by means of bolts not further illustrated. The heat shield 4 also holds a sleeve 5 .
  • a collar 16 on the sleeve 5 locates against the metering panel 1 with pre-tension provided by an interposed spacer 17 .
  • a burner 15 is inserted in the sleeve 5 .
  • this type of combustion chamber head is expensive and difficult to assemble.
  • the cowling 6 must be provided with appropriate assembly openings (not shown) to enable the bolt-type fastenings to be made.
  • the position of the sleeve 5 or the heat shield 4 , respectively, relative to the metering panel 1 is to be adjusted.
  • the heat shield 4 is to be set by means of a washer 18 .
  • FIGS. 2 to 6 illustrate an embodiment according to the present invention.
  • FIG. 2 is a schematic sectional side view showing, in simplified representation, an annular combustion chamber with a combustion chamber outer wall 2 and a combustion chamber inner wall 3 .
  • the metering panel 1 forms one part with the combustion chamber walls 2 and 3 and contains appropriate openings enabling cylindrical rims 13 of a heat shield 4 to be led through (ref. FIGS. 3 and 4 ).
  • the rim 13 of the heat shield 4 extends upstream in the axial direction.
  • a sleeve 5 with an annular collar 14 abuts the rim 13 of the heat shield 4 .
  • the diameter of the collar 14 is designed such that the sleeve 5 can move in the sideward direction relative to the metering panel 1 or the heat shield 4 , respectively, without incurring the risk of undesired cooling air leakage.
  • the heat shield 4 features several stud bolts 7 (of which only some are shown in FIG. 5 for clarity purposes).
  • the stud bolts 7 pass through openings of the metering panel 1 and of the bases of the retainers 8 , thereby providing for a common bolt-type connection of the retainers 8 and of the heat shield 4 to the metering panel 1 .
  • FIG. 6 is a sectional view, similar to FIG. 4, in which the sectional plane is passed through at least one of the stud bolts 7 of the heat shield 4 to elucidate the bolt-type connection of the heat shield 4 to the metering panel 1 by means of the stud bolts 7 with the retainers 8 interposed.
  • each of the retainers 8 features a stud bolt 9 which serves for the attachment of the cowling 6 , as shown in FIG. 4 .
  • the metering panel 1 contains annular grooves 11 (ref. FIG. 5 ), each accommodating a rim 10 of the cowling 6 (FIG. 3 ).
  • the metering panel features a plurality of cooling air holes 12 , as known from the state of the art.
  • the arrangement according to the present invention provides for sufficient spaces to supply cooling air to the heat shield 4 .
  • the combustion chamber head provides for the supply of cooling air to the heat shield 4 through openings in the cowling 6 , both directly via the cooling air holes 12 of the metering panel 1 and, in the area of the sleeve 5 , via the spaces 19 formed by the rim 13 of the heat shield 4 and the collar 14 of the sleeve 5 beneath the retainer 8 through the cooling air holes 12 of the metering panel 1 .
  • the design proposed in the present invention therefore, simplifies the assembly of the sleeves by providing a removable cowling. Furthermore, the cooling air for the heat shield can be supplied closely to the central bore of the heat shield. This provides for efficient cooling of all zones of the heat shield.
  • the present invention also provides for a design of heat shield in which the air mass flow between the heat shield and the metering panel can be passed to the outside via the entire rearward surface of the heat shield, this air being used, on its further route, as starter film for the combustion chamber walls. Accordingly, the benefits of this invention are, on the one hand, the simplified assembly which results in a considerable reduction of costs and, on the other hand, the improved cooling of the heat shield which results in an increase of life and a saving of cooling air.
  • the cooling air which is saved over the state of the art can, for instance, be integrated in the combustion process, this resulting in an additional pollutant reduction.
  • the present invention relates to a combustion chamber head for a gas turbine with at least one combustion chamber wall 2 , 3 , a metering panel 1 , at least one heat shield 4 , at least one sleeve 5 and a cowling 6 , characterized in that the metering panel 1 forms one part with the combustion chamber outer wall 2 and the combustion chamber inner wall 3 , in that the heat shield 4 is mounted onto the metering panel 1 from the downstream side of the metering panel 1 , in that the sleeve 5 is mounted to the metering panel 1 from the upstream side, and in that the cowling 6 is separably (removably) attached to the metering panel 1 .

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Supercharger (AREA)

Abstract

The present invention relates to a combustion chamber head for a gas turbine with at least one combustion chamber wall 2,3, a metering panel 1, at least one heat shield 4, at least one sleeve 5 and a cowling 6, characterized in that the metering panel 1 forms one part with the combustion chamber outer wall 2 and the combustion chamber inner wall 3, in that the heat shield 4 is mounted onto the metering panel 1 from the downstream side of the metering panel 1, in that the sleeve 5 is mounted to the metering panel 1 from the upstream side, and in that the cowling 6 is separably attached to the metering panel 1.

Description

BACKGROUND OF THE INVENTION
This application claims priority to German Patent Application 10048864.1 filed Oct. 2, 2000, which application is incorporated by reference herein.
This invention relates to a gas turbine with at least one combustion chamber, a combustion chamber wall, a metering panel, at least one heat shield, at least one sleeve and a cowling.
Various designs of combustion chamber heads are known in the state of the art. For example, combustion chambers are of the one-part annular type made up of several, inseparably connected components. The main components are the inner and the outer combustion chamber wall and the combustion chamber head. The combustion chamber head is either made as a single component, for example by casting, or of different components, such as sheet-metal fabrications, turned parts etc.
Known combustion chamber heads are taught in Specifications EP 841 520 A2, U.S. Pat. No. 5,524,430, EP 927 854 A2, U.S. Pat. No. 5,289,687 or U.S. Pat. No. 5,331,815.
Besides the one-part designs, combustion chamber heads are known which are made up of individual components joined together by bolt-type fastenings or similar means.
The known designs generally are characterized by a high assembly effort. In particular, assembly of the heat shield together with the sleeves to the metering panel is difficult with some of the known designs since it must be performed from the exit side of the combustion chamber. This involves a considerable increase of the assembly costs.
Furthermore, the known combustion chamber heads have zones which are problematic in terms of the supply of cooling air, these problems arising from the circumstance that the individual components may compromise the supply of cooling air to the heat shield in certain zones.
In the design known from EP 841 520 A2, the sleeve and the heat shield form a unit and are assembled together on the metering panel from the exit of the combustion chamber. In this design, the surface of the sleeve which faces the combustion chamber interior is liable to considerable heating and cannot be cooled effectively.
BRIEF SUMMARY OF THE INVENTION
In a broad aspect, the present invention provides a combustion chamber head of the type specified at the beginning which combines simplicity of design and easy and cost-effective manufacture and assembly with the capability of effective cooling of the heat shield.
It is a particular object of the present invention to provide a combustion chamber head for a gas turbine, comprising: a combustion chamber outer wall; a combustion chamber inner wall; a metering panel; at least one heat shield; at least one sleeve; and a cowling; wherein the metering panel is formed as a unitary part with the combustion chamber outer wall and the combustion chamber inner wall, the heat shield is mounted to the metering panel from a downstream side of the metering panel, the sleeve is mounted to the metering panel from an upstream side of the metering panel, and the cowling is removably attached to the metering panel. Further objects and advantages of the invention will be apparent from the description below.
The combustion chamber head according to this invention is characterized by a variety of merits.
According to the present invention, the heat shield is mounted to the metering panel from the downstream side, whilst all other components are fitted from the upstream side of the metering panel. This method of assembly is far simpler since it dispenses with the need of fitting and securing bolt-type fastenings or similar means from the side of the combustion chamber interior. The removable cowling provides for free, undisturbed access to the assembly areas. Providing the cowling as an extra, removable, separate component enables the entire combustion chamber head to be assembled without any problems. Moreover, it is not necessary to provide the cowling with assembly openings or similar means as known in the prior art. Rather, the present invention provides for free, unhindered access to the upstream side of the metering panel.
A particularly favourable feature of the design according to the present invention is that the sleeves are installed from the upstream side of the metering panel. This feature provides for re-location of the sliding and sealing face away from the metering panel, enabling cooling air to reach also the inner areas of the heat shield without problems. This provides for more effective and improved cooling.
In a particularly favourable development of the present invention, the heat shield is provided with stud bolts which can be led through openings in the metering panel. Separate bolts or similar means are, therefore, dispensable. Attaching the stud bolts to the heat shield also ensures high operational safety by avoiding the risk of parts coming off and entering the combustion chamber interior during operation.
In accordance with the present invention, the sleeve is preferably attached by means of retainers on the metering panel. In a favourable development of the present invention, these retainers are attached to the stud bolts of the heat shield. Additional bolts or threaded fastenings can, therefore, be entirely dispensed with. The entire construction is simplified considerably.
In a particularly favourable arrangement, each retainer holds two adjacent sleeves.
This allows for smaller retainers, with each retainer required to cover only a partial area of the sleeve. This arrangement is also beneficial in terms of the supply of cooling air.
For maximum simplicity of attachment of the cowling, at least one stud bolt is provided on the retainers. Thus, the cowling can simply be put onto the studs and bolted from the exterior.
For attachment and positioning of the cowling it is particularly favourable to locate the rim of the cowling in a groove in the metering panel. This design safely retains and centers the cowling. Furthermore, the groove will restrain the cowling in the case of a bird strike. The restraint provided by this design will, in this case, prevent the simply designed sheet-metal part from plainly bending out by enabling it to transform much more energy into deformation work, thereby reducing the degree of deformation and ensuring the continued operation of the combustion chamber head for the remaining operating time.
According to the present invention, the metering panel is provided with a plurality of cooling air holes, as known in the state of the art.
To improve the cooling of the heat shield, it can be favourable to provide it with a rim which abuts a collar of the sleeve, this rim extending in the upstream direction and being led through an opening in the metering panel. The height of the rim is selected such that, in the installed condition, the rim extends appropriately beyond the upstream side of the metering panel, thereby allowing the cooling air to freely access the central zone of the heat shield even if the collar of the sleeve abuts the cylindrical rim.
The design according to the present invention enables a defined gap to be provided between the outer wall of the cylindrical rim of the sleeve and the inner wall of the rim of the heat shield, this gap permitting a radial and circumferential relative movement of a fuel nozzle and the combustion chamber head. The size of the collar of the sleeve exceeds the outer diameter of the rim of the heat shield by the max. possible amount of movement, this feature enabling the space before the metering panel to be sealed to the combustion chamber against undesired leakage air even if the max. possible movement of the sleeve should take place. This provides for advantageous assembly and operating conditions.
Furthermore, the gaps between the sleeve and the retainers are particularly advantageous since they provide for sufficient clearance necessary for thermal compensation. On the other hand, provision is made for the secure positioning of the sleeve. The sleeve is securely and adequately positioned by the left or right part, respectively, of the adjacent retainers. Accordingly, each retainer secures two adjacent sleeves. As already mentioned, the retainer itself is fitted to the stud bolts of the heat shield and secured to the metering panel with appropriate nuts. In accordance with this invention, the retainer can accordingly also be designed as a support for the cowling, as already mentioned in the above.
The design proposed in the present invention enables the individual components to be separately manufactured and safely assembled. This provides for a high degree of flexibility also in terms of the candidate manufacturing processes and materials.
BRIEF DESCRIPTION OF THE DRAWINGS
The invention is more fully described in the light of the accompanying drawings showing an embodiment of the present invention. On the drawings:
FIG. 1 is a design of a combustion chamber head in accordance with the state of the art,
FIG. 2 is a simplified sectional side view of an embodiment of a combustion chamber according to the present invention with a combustion chamber head according to the present invention,
FIG. 3 is an enlarged partial view of the combustion chamber head of FIG. 2,
FIG. 4 is a sectional view of a combustion chamber head showing multiple heat shields and sleeves,
FIG. 5 is a perspective partial view similar to FIG. 4 of the upstream area of the metering panel with the multiple sleeves and retainers, and
FIG. 6 is a simplified sectional side view of the metering panel and the heat shield showing the attachment of the heat shield by means of stud bolts.
DETAILED DESCRIPTION OF THE INVENTION
FIG. 1 shows the design according to the state of the art in which a combustion chamber outer wall 2 and a combustion chamber inner wall 3 forms a one-part design with a metering panel 1. Also, the metering panel 1 forms one part with a cowling 6. A heat shield 4 is fastened to the metering panel by means of bolts not further illustrated. The heat shield 4 also holds a sleeve 5. A collar 16 on the sleeve 5 locates against the metering panel 1 with pre-tension provided by an interposed spacer 17. A burner 15 is inserted in the sleeve 5.
Apparently, this type of combustion chamber head is expensive and difficult to assemble. The cowling 6 must be provided with appropriate assembly openings (not shown) to enable the bolt-type fastenings to be made. Furthermore, the position of the sleeve 5 or the heat shield 4, respectively, relative to the metering panel 1 is to be adjusted. For this purpose, the heat shield 4 is to be set by means of a washer 18.
FIGS. 2 to 6 illustrate an embodiment according to the present invention.
FIG. 2 is a schematic sectional side view showing, in simplified representation, an annular combustion chamber with a combustion chamber outer wall 2 and a combustion chamber inner wall 3. The metering panel 1 forms one part with the combustion chamber walls 2 and 3 and contains appropriate openings enabling cylindrical rims 13 of a heat shield 4 to be led through (ref. FIGS. 3 and 4).
As becomes apparent from the illustrations in FIGS. 3 and 4, in particular, the rim 13 of the heat shield 4 extends upstream in the axial direction. A sleeve 5 with an annular collar 14 abuts the rim 13 of the heat shield 4. As already mentioned, the diameter of the collar 14 is designed such that the sleeve 5 can move in the sideward direction relative to the metering panel 1 or the heat shield 4, respectively, without incurring the risk of undesired cooling air leakage.
As becomes apparent from FIG. 5, in particular, the heat shield 4 features several stud bolts 7 (of which only some are shown in FIG. 5 for clarity purposes). The stud bolts 7 pass through openings of the metering panel 1 and of the bases of the retainers 8, thereby providing for a common bolt-type connection of the retainers 8 and of the heat shield 4 to the metering panel 1.
FIG. 6 is a sectional view, similar to FIG. 4, in which the sectional plane is passed through at least one of the stud bolts 7 of the heat shield 4 to elucidate the bolt-type connection of the heat shield 4 to the metering panel 1 by means of the stud bolts 7 with the retainers 8 interposed.
In their centric area, each of the retainers 8 features a stud bolt 9 which serves for the attachment of the cowling 6, as shown in FIG. 4.
The metering panel 1 contains annular grooves 11 (ref. FIG. 5), each accommodating a rim 10 of the cowling 6 (FIG. 3).
As becomes apparent from FIG. 4, the metering panel features a plurality of cooling air holes 12, as known from the state of the art. The arrangement according to the present invention provides for sufficient spaces to supply cooling air to the heat shield 4.
As becomes apparent from the Figures, the combustion chamber head according to the present invention provides for the supply of cooling air to the heat shield 4 through openings in the cowling 6, both directly via the cooling air holes 12 of the metering panel 1 and, in the area of the sleeve 5, via the spaces 19 formed by the rim 13 of the heat shield 4 and the collar 14 of the sleeve 5 beneath the retainer 8 through the cooling air holes 12 of the metering panel 1.
The design proposed in the present invention, therefore, simplifies the assembly of the sleeves by providing a removable cowling. Furthermore, the cooling air for the heat shield can be supplied closely to the central bore of the heat shield. This provides for efficient cooling of all zones of the heat shield. The present invention also provides for a design of heat shield in which the air mass flow between the heat shield and the metering panel can be passed to the outside via the entire rearward surface of the heat shield, this air being used, on its further route, as starter film for the combustion chamber walls. Accordingly, the benefits of this invention are, on the one hand, the simplified assembly which results in a considerable reduction of costs and, on the other hand, the improved cooling of the heat shield which results in an increase of life and a saving of cooling air. The cooling air which is saved over the state of the art can, for instance, be integrated in the combustion process, this resulting in an additional pollutant reduction.
Generally, a plurality of modifications may be made to the embodiment shown without departing from the inventive concept expressed.
Summarizing, then,
the present invention relates to a combustion chamber head for a gas turbine with at least one combustion chamber wall 2,3, a metering panel 1, at least one heat shield 4, at least one sleeve 5 and a cowling 6, characterized in that the metering panel 1 forms one part with the combustion chamber outer wall 2 and the combustion chamber inner wall 3, in that the heat shield 4 is mounted onto the metering panel 1 from the downstream side of the metering panel 1, in that the sleeve 5 is mounted to the metering panel 1 from the upstream side, and in that the cowling 6 is separably (removably) attached to the metering panel 1.
LIST OF REFERENCE NUMERALS
1 Metering panel
2 Combustion chamber outer wall
3 Combustion chamber inner wall
4 Heat shield
5 Sleeve
6 Cowling
7 Stud bolt of 4
8 Retainer
9 Stud bolt of 8
10 Rim of 6
11 Groove of 1
12 Cooling air hole of 1
13 Rim of 4
14 Collar of 5
15 Burner
16 Collar
17 Spacer
18 Washer
19 Space

Claims (23)

What is claimed is:
1. A combustion chamber head for a gas turbine, comprising:
a combustion chamber outer wall;
a combustion chamber inner wall;
a metering panel;
at least one heat shield;
at least one sleeve; and
a cowling;
wherein the metering panel is formed as a unitary part with the combustion chamber outer wall and the combustion chamber inner wall, the heat shield is mounted to the metering panel from a downstream side of the metering panel, the sleeve is mounted to the metering panel from an upstream side of the metering panel, and the cowling is removably attached to the metering panel, and further comprising a plurality of retainers and a plurality of sleeves, with each retainer attaching two adjacent sleeves to the metering panel.
2. The combustion chamber head of claim 1, wherein the heat shield includes a plurality of stud bolts which can be inserted through openings in the metering panel.
3. The combustion chamber head of claim 2, wherein the retainer is attached to the stud bolts of the heat shield.
4. The combustion chamber head of claim 3, wherein each retainer includes at least one stud bolt for attaching the cowling.
5. The combustion chamber head of claim 4, wherein the metering panel includes a groove to accommodate a rim of the cowling.
6. The combustion chamber head of claim 5, wherein the metering panel includes a plurality of cooling air holes from the upstream side to the downstream side.
7. The combustion chamber head of claim 6, wherein the heat shield includes a rim which abuts a collar of the sleeve, the rim extending in an upstream direction through an opening in the metering panel.
8. The combustion chamber head of claim 7, wherein a height of the rim is sized to provide a cooling air passage space for cooling the heat shield.
9. The combustion chamber head of claim 8, wherein cooling air is routed through openings in the cowling to the heat shield via the cooling air holes in the metering panel and, in the area of the sleeve, through the cooling air passage space formed by the rim of the heat shield and a collar of the sleeve beneath the retainer and via the cooling air holes in the metering panel, the cooling air also being used downstream as a starter film for cooling at least one of the combustion chamber walls.
10. The combustion chamber head of claim 1, wherein the metering panel includes a groove to accommodate a rim of the cowling.
11. The combustion chamber head of claim 10, wherein the heat shield includes a rim which abuts a collar of the sleeve, the rim extending in an upstream direction through an opening in the metering panel.
12. The combustion chamber head of claim 11, wherein cooling air is routed through openings in the cowling to the heat shield via the cooling air holes in the metering panel and, in the area of the sleeve, through a cooling air passage space formed by the rim of the heat shield and a collar of the sleeve and via the cooling air holes in the metering panel, the cooling air also being used downstream as a starter film for cooling at least one of the combustion chamber walls.
13. The combustion chamber head of claim 1, wherein the heat shield includes a rim which abuts a collar of the sleeve, the rim extending in an upstream direction through an opening in the metering panel.
14. The combustion chamber head of claim 13, wherein cooling air is routed through openings in the cowling to the heat shield via cooling air holes in the metering panel and, in the area of the sleeve, through a cooling air passage space formed by the rim of the heat shield and a collar of the sleeve and via the cooling air holes in the metering panel, the cooling air also being used downstream as a starter film for cooling at least one of the combustion chamber walls.
15. A combustion chamber head for a gas turbine, comprising:
a combustion chamber outer wall;
a combustion chamber inner wall;
a metering panel;
at least one heat shield;
at least one sleeve; and p1 a cowling;
wherein the metering panel is formed as a unitary part with the combustion chamber outer wall and the combustion chamber inner wall, the heat shield is mounted to the metering panel from a downstream side of the metering panel, the sleeve is mounted to the metering panel from an upstream side of the metering panel, and the cowling is removably attached to the metering panel, the metering panel including a radially outer groove and a radially inner groove, the radially outer groove engaging substantially an entire circumference of both an inner and outer surface of a radially outer rim of the cowling and the radially inner groove engaging substantially an entire circumference of both an inner and outer surface of a radially inner rim of the cowling.
16. The combustion chamber head of claim 15, wherein the heat shield includes a plurality of stud bolts which can be inserted through openings in the metering panel.
17. The combustion chamber head of claim 16, wherein the retainer is attached to the stud bolts of the heat shield.
18. The combustion chamber head of claim 15, wherein the heat shield includes a rim which abuts a collar of the sleeve, the rim extending in an upstream direction through an opening in the metering panel.
19. The combustion chamber head of claim 18, wherein a height of the rim is sized to provide a cooling air passage space for cooling the heat shield.
20. The combustion chamber head of claim 19, wherein cooling air is routed through openings in the cowling to the heat shield via the cooling air holes in the metering panel and, in the area of the sleeve, through the cooling air passage space formed by the rim of the heat shield and a collar of the sleeve beneath the retainer and via the cooling air holes in the metering panel, the cooling air also being used downstream as a starter film for cooling at least one of the combustion chamber walls.
21. The combustion chamber head of claim 15, and further comprising a plurality of retainers and a plurality of sleeves, with each retainer attaching two adjacent sleeves to the metering panel.
22. The combustion chamber head of claim 21, wherein each retainer includes at least one stud bolt for attaching the cowling.
23. The combustion chamber head of claim 15, wherein the sleeve is attached to the metering panel with at least one retainer and each retainer includes at least one stud bolt for attaching the cowling.
US09/968,491 2000-10-02 2001-10-02 Combustion chamber head for a gas turbine Expired - Lifetime US6679063B2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10048864.1 2000-10-02
DE10048864 2000-10-02
DE10048864A DE10048864A1 (en) 2000-10-02 2000-10-02 Combustion chamber head for a gas turbine

Publications (2)

Publication Number Publication Date
US20020038549A1 US20020038549A1 (en) 2002-04-04
US6679063B2 true US6679063B2 (en) 2004-01-20

Family

ID=7658490

Family Applications (1)

Application Number Title Priority Date Filing Date
US09/968,491 Expired - Lifetime US6679063B2 (en) 2000-10-02 2001-10-02 Combustion chamber head for a gas turbine

Country Status (3)

Country Link
US (1) US6679063B2 (en)
EP (1) EP1193451B1 (en)
DE (2) DE10048864A1 (en)

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060042271A1 (en) * 2004-08-27 2006-03-02 Pratt & Whitney Canada Corp. Combustor and method of providing
US20080115499A1 (en) * 2006-11-17 2008-05-22 Patel Bhawan B Combustor heat shield with variable cooling
US20080115506A1 (en) * 2006-11-17 2008-05-22 Patel Bhawan B Combustor liner and heat shield assembly
US20080115498A1 (en) * 2006-11-17 2008-05-22 Patel Bhawan B Combustor liner and heat shield assembly
US20080229750A1 (en) * 2007-03-22 2008-09-25 Rolls-Royce Plc Location ring arrangement
US20080236169A1 (en) * 2007-03-30 2008-10-02 Eduardo Hawie Combustor floating collar with louver
US20080282703A1 (en) * 2007-05-16 2008-11-20 Oleg Morenko Interface between a combustor and fuel nozzle
US20110000216A1 (en) * 2009-07-06 2011-01-06 Kawasaki Jukogyo Kabushiki Kaisha Gas turbine combustor
US20110265483A1 (en) * 2009-10-28 2011-11-03 Man Diesel & Turbo Se Combustor For A Turbine, and Gas Turbine Outfitted With A Combustor of This Kind
US20140318148A1 (en) * 2013-04-30 2014-10-30 Rolls-Royce Deutschland Ltd & Co Kg Burner seal for gas-turbine combustion chamber head and heat shield
US8943835B2 (en) * 2010-05-10 2015-02-03 General Electric Company Gas turbine engine combustor with CMC heat shield and methods therefor
US9021812B2 (en) 2012-07-27 2015-05-05 Honeywell International Inc. Combustor dome and heat-shield assembly
US9021675B2 (en) 2011-08-15 2015-05-05 United Technologies Corporation Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology
US9222675B2 (en) 2011-03-24 2015-12-29 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber head with holding means for seals on burners in gas turbines
US20160010869A1 (en) * 2014-07-09 2016-01-14 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine with bolted combustion chamber head
US9328926B2 (en) 2011-03-22 2016-05-03 Rolls-Royce Deutschland Ltd & Co Kg Segmented combustion chamber head
US20170167731A1 (en) * 2015-12-11 2017-06-15 Rolls Royce Deutschland Ltd & Co Kg Method for mounting a combustion chamber of a gas turbine engine
US20170176004A1 (en) * 2015-12-18 2017-06-22 Pratt & Whitney Canada Corp. Combustor floating collar assembly
US9803869B2 (en) 2014-03-11 2017-10-31 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber and method for manufacturing the same
US9958159B2 (en) 2013-03-13 2018-05-01 Rolls-Royce Corporation Combustor assembly for a gas turbine engine
US20180356095A1 (en) * 2017-03-06 2018-12-13 General Electric Company Combustion Section of a Gas Turbine Engine
US10378775B2 (en) 2012-03-23 2019-08-13 Pratt & Whitney Canada Corp. Combustor heat shield
US10408456B2 (en) * 2015-10-29 2019-09-10 Rolls-Royce Plc Combustion chamber assembly
US10859271B2 (en) 2017-09-22 2020-12-08 Rolls-Royce Plc Combustion chamber
US11428410B2 (en) 2019-10-08 2022-08-30 Rolls-Royce Corporation Combustor for a gas turbine engine with ceramic matrix composite heat shield and seal retainer
US11466858B2 (en) 2019-10-11 2022-10-11 Rolls-Royce Corporation Combustor for a gas turbine engine with ceramic matrix composite sealing element
US11892165B2 (en) 2021-05-19 2024-02-06 General Electric Company Heat shield for fuel nozzle
US12123592B2 (en) 2022-01-12 2024-10-22 General Electric Company Fuel nozzle and swirler

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9188341B2 (en) * 2008-04-11 2015-11-17 General Electric Company Fuel nozzle
DE102013222863A1 (en) 2013-11-11 2015-05-13 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustor and method for its production
DE102015212573A1 (en) * 2015-07-06 2017-01-12 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustor with integrated turbine guide wheel and method for its production
DE102015213629A1 (en) 2015-07-20 2017-01-26 Rolls-Royce Deutschland Ltd & Co Kg Cover member and combustion chamber assembly for a gas turbine
GB201701380D0 (en) 2016-12-20 2017-03-15 Rolls Royce Plc A combustion chamber and a combustion chamber fuel injector seal
US10378770B2 (en) * 2017-01-27 2019-08-13 General Electric Company Unitary flow path structure
CN107575889B (en) * 2017-09-05 2023-05-16 中国联合重型燃气轮机技术有限公司 Fuel nozzle of gas turbine
US10823419B2 (en) * 2018-03-01 2020-11-03 General Electric Company Combustion system with deflector
US11125436B2 (en) * 2019-07-03 2021-09-21 Pratt & Whitney Canada Corp. Combustor floating collar mounting arrangement
FR3112382B1 (en) * 2020-07-10 2022-09-09 Safran Aircraft Engines ANNULAR COMBUSTION CHAMBER FOR AN AIRCRAFT TURBOMACHINE

Citations (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2944139A1 (en) 1978-11-03 1980-05-14 Gen Electric BURNER ARRANGEMENT
US4262486A (en) * 1978-08-19 1981-04-21 Rolls-Royce Limited Combustion chambers
GB2073401A (en) 1980-04-02 1981-10-14 United Technologies Corp Fuel nozzle guide heatshield for a gas turbine engine
GB2107448A (en) 1980-10-21 1983-04-27 Rolls Royce Gas turbine engine combustion chambers
US4458479A (en) * 1981-10-13 1984-07-10 General Motors Corporation Diffuser for gas turbine engine
GB2247522A (en) 1990-09-01 1992-03-04 Rolls Royce Plc Gas turbine engine combustor
US5129231A (en) 1990-03-12 1992-07-14 United Technologies Corporation Cooled combustor dome heatshield
DE4131069A1 (en) 1991-01-22 1992-07-23 Gen Electric COMBUSTION CHAMBER
US5289687A (en) 1992-03-30 1994-03-01 General Electric Company One-piece cowl for a double annular combustor
EP0604021A1 (en) 1992-12-21 1994-06-29 United Technologies Corporation Individually removable combustor liner panel for a gas turbine engine
US5331815A (en) 1992-03-23 1994-07-26 General Electric Company Impact resistant combustor
US5419115A (en) 1994-04-29 1995-05-30 United Technologies Corporation Bulkhead and fuel nozzle guide assembly for an annular combustion chamber
US5524430A (en) 1992-01-28 1996-06-11 Societe National D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. Gas-turbine engine with detachable combustion chamber
DE19515537A1 (en) 1995-04-27 1996-10-31 Bmw Rolls Royce Gmbh Head part of a gas turbine annular combustion chamber
US5623827A (en) * 1995-01-26 1997-04-29 General Electric Company Regenerative cooled dome assembly for a gas turbine engine combustor
EP0841520A2 (en) 1996-11-07 1998-05-13 ROLLS-ROYCE plc Gas turbine engine combustor
EP0927854A2 (en) 1997-12-31 1999-07-07 United Technologies Corporation Low nox combustor for gas turbine engine
US5924288A (en) 1994-12-22 1999-07-20 General Electric Company One-piece combustor cowl
US5956955A (en) 1994-08-01 1999-09-28 Bmw Rolls-Royce Gmbh Heat shield for a gas turbine combustion chamber
US6412272B1 (en) * 1998-12-29 2002-07-02 United Technologies Corporation Fuel nozzle guide for gas turbine engine and method of assembly/disassembly

Patent Citations (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4262486A (en) * 1978-08-19 1981-04-21 Rolls-Royce Limited Combustion chambers
GB2034874A (en) 1978-11-03 1980-06-11 Gen Electric Gas turbine engine combustor
DE2944139A1 (en) 1978-11-03 1980-05-14 Gen Electric BURNER ARRANGEMENT
GB2073401A (en) 1980-04-02 1981-10-14 United Technologies Corp Fuel nozzle guide heatshield for a gas turbine engine
GB2107448A (en) 1980-10-21 1983-04-27 Rolls Royce Gas turbine engine combustion chambers
US4458479A (en) * 1981-10-13 1984-07-10 General Motors Corporation Diffuser for gas turbine engine
US5129231A (en) 1990-03-12 1992-07-14 United Technologies Corporation Cooled combustor dome heatshield
GB2247522A (en) 1990-09-01 1992-03-04 Rolls Royce Plc Gas turbine engine combustor
DE4131069A1 (en) 1991-01-22 1992-07-23 Gen Electric COMBUSTION CHAMBER
US5142871A (en) 1991-01-22 1992-09-01 General Electric Company Combustor dome plate support having uniform thickness arcuate apex with circumferentially spaced coolant apertures
US5524430A (en) 1992-01-28 1996-06-11 Societe National D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. Gas-turbine engine with detachable combustion chamber
US5331815A (en) 1992-03-23 1994-07-26 General Electric Company Impact resistant combustor
US5289687A (en) 1992-03-30 1994-03-01 General Electric Company One-piece cowl for a double annular combustor
EP0604021A1 (en) 1992-12-21 1994-06-29 United Technologies Corporation Individually removable combustor liner panel for a gas turbine engine
US5419115A (en) 1994-04-29 1995-05-30 United Technologies Corporation Bulkhead and fuel nozzle guide assembly for an annular combustion chamber
US5956955A (en) 1994-08-01 1999-09-28 Bmw Rolls-Royce Gmbh Heat shield for a gas turbine combustion chamber
US5924288A (en) 1994-12-22 1999-07-20 General Electric Company One-piece combustor cowl
US5623827A (en) * 1995-01-26 1997-04-29 General Electric Company Regenerative cooled dome assembly for a gas turbine engine combustor
DE19515537A1 (en) 1995-04-27 1996-10-31 Bmw Rolls Royce Gmbh Head part of a gas turbine annular combustion chamber
US5996335A (en) 1995-04-27 1999-12-07 Bmw Rolls-Royce Gmbh Head part of an annular combustion chamber of a gas turbine having a holding part to secure a burner collar in a bayonet-catch type manner
EP0841520A2 (en) 1996-11-07 1998-05-13 ROLLS-ROYCE plc Gas turbine engine combustor
EP0927854A2 (en) 1997-12-31 1999-07-07 United Technologies Corporation Low nox combustor for gas turbine engine
US6412272B1 (en) * 1998-12-29 2002-07-02 United Technologies Corporation Fuel nozzle guide for gas turbine engine and method of assembly/disassembly

Cited By (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7308794B2 (en) * 2004-08-27 2007-12-18 Pratt & Whitney Canada Corp. Combustor and method of improving manufacturing accuracy thereof
US20060042271A1 (en) * 2004-08-27 2006-03-02 Pratt & Whitney Canada Corp. Combustor and method of providing
US7721548B2 (en) 2006-11-17 2010-05-25 Pratt & Whitney Canada Corp. Combustor liner and heat shield assembly
US20080115499A1 (en) * 2006-11-17 2008-05-22 Patel Bhawan B Combustor heat shield with variable cooling
US20080115506A1 (en) * 2006-11-17 2008-05-22 Patel Bhawan B Combustor liner and heat shield assembly
US20080115498A1 (en) * 2006-11-17 2008-05-22 Patel Bhawan B Combustor liner and heat shield assembly
US7748221B2 (en) 2006-11-17 2010-07-06 Pratt & Whitney Canada Corp. Combustor heat shield with variable cooling
US7681398B2 (en) 2006-11-17 2010-03-23 Pratt & Whitney Canada Corp. Combustor liner and heat shield assembly
US20080229750A1 (en) * 2007-03-22 2008-09-25 Rolls-Royce Plc Location ring arrangement
US20080236169A1 (en) * 2007-03-30 2008-10-02 Eduardo Hawie Combustor floating collar with louver
US7861530B2 (en) * 2007-03-30 2011-01-04 Pratt & Whitney Canada Corp. Combustor floating collar with louver
US7926280B2 (en) * 2007-05-16 2011-04-19 Pratt & Whitney Canada Corp. Interface between a combustor and fuel nozzle
US20080282703A1 (en) * 2007-05-16 2008-11-20 Oleg Morenko Interface between a combustor and fuel nozzle
US8511088B2 (en) * 2009-07-06 2013-08-20 Kawasaki Jukogyo Kabushiki Kaisha Gas turbine fuel injector mounting system
US20110000216A1 (en) * 2009-07-06 2011-01-06 Kawasaki Jukogyo Kabushiki Kaisha Gas turbine combustor
EP2317227B1 (en) * 2009-10-28 2019-10-02 MAN Energy Solutions SE Burner for a turbine and gas turbine with same
US20110265483A1 (en) * 2009-10-28 2011-11-03 Man Diesel & Turbo Se Combustor For A Turbine, and Gas Turbine Outfitted With A Combustor of This Kind
US9140452B2 (en) * 2009-10-28 2015-09-22 Man Diesel & Turbo Se Combustor head plate assembly with impingement
US8943835B2 (en) * 2010-05-10 2015-02-03 General Electric Company Gas turbine engine combustor with CMC heat shield and methods therefor
US9964309B2 (en) 2010-05-10 2018-05-08 General Electric Company Gas turbine engine combustor with CMC heat shield and methods therefor
US9328926B2 (en) 2011-03-22 2016-05-03 Rolls-Royce Deutschland Ltd & Co Kg Segmented combustion chamber head
US9222675B2 (en) 2011-03-24 2015-12-29 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber head with holding means for seals on burners in gas turbines
US9021675B2 (en) 2011-08-15 2015-05-05 United Technologies Corporation Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology
US9995487B2 (en) 2011-08-15 2018-06-12 United Technologies Corporation Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology
US10378775B2 (en) 2012-03-23 2019-08-13 Pratt & Whitney Canada Corp. Combustor heat shield
US9021812B2 (en) 2012-07-27 2015-05-05 Honeywell International Inc. Combustor dome and heat-shield assembly
US9958159B2 (en) 2013-03-13 2018-05-01 Rolls-Royce Corporation Combustor assembly for a gas turbine engine
US10041415B2 (en) * 2013-04-30 2018-08-07 Rolls-Royce Deutschland Ltd & Co Kg Burner seal for gas-turbine combustion chamber head and heat shield
US20140318148A1 (en) * 2013-04-30 2014-10-30 Rolls-Royce Deutschland Ltd & Co Kg Burner seal for gas-turbine combustion chamber head and heat shield
US9803869B2 (en) 2014-03-11 2017-10-31 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber and method for manufacturing the same
US10012390B2 (en) * 2014-07-09 2018-07-03 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine with bolted combustion chamber head
US20160010869A1 (en) * 2014-07-09 2016-01-14 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine with bolted combustion chamber head
US10408456B2 (en) * 2015-10-29 2019-09-10 Rolls-Royce Plc Combustion chamber assembly
US10544942B2 (en) * 2015-12-11 2020-01-28 Rolls-Royce Deutschland Ltd & Co Kg Method for mounting a combustion chamber of a gas turbine engine
US20170167731A1 (en) * 2015-12-11 2017-06-15 Rolls Royce Deutschland Ltd & Co Kg Method for mounting a combustion chamber of a gas turbine engine
US20170176004A1 (en) * 2015-12-18 2017-06-22 Pratt & Whitney Canada Corp. Combustor floating collar assembly
US20180356095A1 (en) * 2017-03-06 2018-12-13 General Electric Company Combustion Section of a Gas Turbine Engine
CN110582674A (en) * 2017-03-06 2019-12-17 通用电气公司 Combustion section of a gas turbine engine
US10837640B2 (en) * 2017-03-06 2020-11-17 General Electric Company Combustion section of a gas turbine engine
CN110582674B (en) * 2017-03-06 2021-06-22 通用电气公司 Combustion section of a gas turbine engine
US10859271B2 (en) 2017-09-22 2020-12-08 Rolls-Royce Plc Combustion chamber
US11428410B2 (en) 2019-10-08 2022-08-30 Rolls-Royce Corporation Combustor for a gas turbine engine with ceramic matrix composite heat shield and seal retainer
US11466858B2 (en) 2019-10-11 2022-10-11 Rolls-Royce Corporation Combustor for a gas turbine engine with ceramic matrix composite sealing element
US11892165B2 (en) 2021-05-19 2024-02-06 General Electric Company Heat shield for fuel nozzle
US12123592B2 (en) 2022-01-12 2024-10-22 General Electric Company Fuel nozzle and swirler

Also Published As

Publication number Publication date
EP1193451A2 (en) 2002-04-03
US20020038549A1 (en) 2002-04-04
DE50105179D1 (en) 2005-03-03
EP1193451A3 (en) 2002-05-15
EP1193451B1 (en) 2005-01-26
DE10048864A1 (en) 2002-04-11

Similar Documents

Publication Publication Date Title
US6679063B2 (en) Combustion chamber head for a gas turbine
US6497105B1 (en) Low cost combustor burner collar
US5996335A (en) Head part of an annular combustion chamber of a gas turbine having a holding part to secure a burner collar in a bayonet-catch type manner
EP2224102B1 (en) A coolable shroud seal segment assembly of a gas turbine engine
US7581402B2 (en) Turbine engine combustor with bolted swirlers
US9097141B2 (en) Axial bolting arrangement for mid turbine frame
EP2844854B1 (en) Annular gas turbine engine combustor liner and method of controlling its movement
US5577379A (en) Fuel nozzle guide retainer assembly
JPH0229938B2 (en)
US9506653B2 (en) Combustion chamber of a gas turbine
EP0797746B1 (en) Bulkhead liner with raised lip
US4466240A (en) Fuel nozzle for gas turbine engine with external and internal removal capability
NO300343B1 (en) Burner hood unit with low NOx emissions
EP3039344B1 (en) Swirler mount interface for a gas turbine engine combustor
US20150260402A1 (en) Combustion chamber of a gas turbine
US20120272662A1 (en) Head part of an annular combustion chamber
JP3998494B2 (en) Replaceable afterburner heat shield
US20040159107A1 (en) Combustion liner cap assembly attachment and sealing system
EP3760927B1 (en) Gas turbine engine combustor
JP3697093B2 (en) Gas turbine combustor
CN111836998B (en) Double-chamber bottom of combustion chamber
US20180017260A1 (en) Combustor anti-surge retention system
US20170023250A1 (en) Cowling part and combustor assembly for a gas turbine
CA2499258C (en) Combustor assembly and method
JP2004177108A (en) Combustor for burning inflammable fluid mixture

Legal Events

Date Code Title Description
AS Assignment

Owner name: ROLLS-ROYCE DEUTSCHLAND LTD. & CO KG, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:EBEL, MICHAEL;REEL/FRAME:012225/0419

Effective date: 20010921

STCF Information on status: patent grant

Free format text: PATENTED CASE

FEPP Fee payment procedure

Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

FPAY Fee payment

Year of fee payment: 4

FPAY Fee payment

Year of fee payment: 8

FPAY Fee payment

Year of fee payment: 12

SULP Surcharge for late payment

Year of fee payment: 11